U/A Canada PT6A-42
Service difficulty reports · 396
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'PT6A42' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'PT6A42' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AUS20030319Hub · cracked(AUS) PROPELLER HUB CONTAINED A RADIAL CRACK IN THE OUTBOARD END OF THE NR 1 HUB ARM AT THE HUB/PILOT TUBE JOINT. CRACK WAS CONFIRMEDUSING MAGNETIC PARTICLE INSPECTION (MPI). CRACK LENGTH APPROXIMATELY 25.4MM (1IN). FOUND DURING DISASSEMBLY AND INSPECTION FOLLSDR CA030218001Spar Cap · corroded(CAN) CORROSION ON UPPER RIGHT AND LEFT FORWARD WING SPAR CAPS BETWEEN WS 223 & 236 AND WS 122 & 132. CORROSION IS BEYOND LIMITS, WINGS TO BE REMOVED AND SPARS TO BE REPLACED AS DIRECTED BY BEECHCRAFT ENGINEERING.SDR CA030129004Coax · unserviceable(CAN) DURING AIRCRAFT IMPORTATION INSPECTION INTO CANADA, AVIONICS CHECKS NOTED WEAK NAVIGATION, COMMS, G/S RECEPTION. TROUBLESHOOTING FOUND THAT THE COAXIAL CABLE INSTALLED FOR THE ENTIRE AIRCRAFT, NAVIGATION, AND COMMUNICATIONS SYSTEMS HAD A MANUFACTURING DSDR CA030124004Shaft · sheared(CAN) AT ENGINE START UP, THE PROPELLER WOULD NOT COME OUT OF FEATHER. INSPECTION REVEALED A SHEARED CONSTANT SPEED PROPELLER GOVERNOR SHAFT.SDR CA030107014Actuator · noisy(CAN) AFTER HAVING PROBLEMS WITH A LOW TIME ACTUATORS ON TWO OTHER AIRCRAFT, WE DECIDED TO CHECK ALL ACTUATOR THAT WERE OVERHAULED BY THAT SUPPLIER.DURING SPECIAL INSPECTION OF THIS ACTUATOR, WE FOUND THAT THE LANDING GEAR ACTUATOR WAS SQUEALING DURING GEAR EXSDR CA030106002Fuse · blown(CAN) FUSE (GMW1) HAS POPPED ON THREE DIFFERENT COMPANY B200 AIRCRAFT. FUSE PROJECTS 28 VDC OUTPUT CIRCUIT FROM THE EFIS STANDBY POWER SUPPLY (WIRES W3203-2 AND W3204-4). HAVE SUBMITTED QUERY TO RAYTHEON TECH SUPPORT FOR RECTIFICATION.SDR AUS20021341Fitting · cracked(AUS) REAR PRESSURE BULKHEAD STIFFENER CLEAT CRACKED. CLEAT IS FITTED AS PART OF CARGO DOOR MODIFICATION. FOUND DURING INSPECTION IAW AD/BEECH200/55 (SB/2472).SDR AUS20021330Bulkhead · damaged(AUS) REAR PRESSURE BULKHEAD DAMAGED. PUNCTURE HOLE IN BULKHEAD WEB LOCATED IN AREA BETWEEN THE CENTRELINE AND INBOARD OF THE OVERPRESSURE AND OUTFLOW VALVE CUTOUT. FOUND DURING INSPECTIONIAW RAYTHEON SB/53/3513 REV1. DAMAGE CAUSED DUE TO IMPACT BYTRIM.SDR CA021118005Carbon Seal · failed(CAN) PILOT NOTICED SLIGHT OIL PRESSURE FLUCTUATION OF THE RT ENGINE DURING A TRAINING FLIGHT AND RETURNED TO BASE. OIL LOSS CONFIRMED AND DETERMINED THAT THE OIL (4 LITERS) HAD EXITED THROUGH THE ENGINE BREATHER SYSTEM. REMOVED ACCESSORY GEARBOX AND REPLACED SDR AUS20021234Torque Tube · faulty(AUS) RUDDER TORQUE TUBE RIVETS LOOSE AND RIVET HOLES WORN BY UP TO APPROXIMATELY 0.254MM (0.010IN) OVERSIZE.SDR BN001Strap · crackedUPON REMOVAL OF AIRCRAFT INTERIOR TO TROUBLESHOOT WIRING PROBLEMS, TWO STRAP ASSEMBLIES ON THE RT SIDE OF THE FUSELAGE AT F.S. 227.0 AND 246.0, BUTTOCK LINE 119.0 WERE FOUND COMPLETELY CRACKED THROUGH. THE STRAP ASSEMBLY AT F.S. 246.0. THESE AREAS WOULD NOTSDR AUS20021211Arm · worn(AUS) RUDDER PEDAL PIVOT ARM WORN AND FINALLY FAILED IN AREA OF PIVOT BUSHES.SDR CA021104010Hinge · cracked(CAN) UPON INSPECTION IT WAS NOTED THAT THE DOOR ASSY BYPASS ICE VANE WAS RUBBING AGAINST THE COWLING. AFTER CLOSE INSPECTION IT WAS NOTED THAT THE HINGE HAD CRACKED FROM THE INBOARD END OUTBOARD ABOUT 3 INCH ALONG THE HINGE PIN. THE HINGE ASSEMBLY WAS REPLACSDR CA021018001Rivet · corroded(CAN) DURING UNSCHEDULED MAINTENANCE, RIVET HEADS WERE FOUND SITTING ON THE FRAME BELOW THE WINDOW, AFTER FURTHER INVESTIGATION FOUND THAT THE RIVET HEADS CAME FROM THE SPLICE IN THE CHANNEL AT STA 193.00. RIVET HEADS WERE CORRODED AND SEPARATED WITH HALF OFSDR AUS20021078Engine · seized(AUS) RT ENGINE SUFFERED AN IN FLIGHT FAILURE WITH THE ENGINE SEIZING. INSPECTION FOUND A CRACK IN THE COMPRESSOR SECTION INTAKE HOUSING WITH OIL POOLING IN THE EXHAUST SECTION. CRACK LENGTH 50.8MM TO 63.5MM (2IN TO 2.5IN).SDR CA021001006Windshield · overheated(CAN) SHORTED AND OVERHEAT CONDITION ON LT WINDSHIELD GROUND TERMINAL CAUSING A HEAVY SMELL OF BURNED PLEXIGLASS TYPE OF ODOUR. PILOTS SWITCHED OFF LT WINDSHIELD ANTI-ICE AND SMOLDERING SUBSIDED.SDR AUS20021052Handle · sheared(AUS) PRIOR TO FLIGHT THE PILOT WAS CLOSING THE AIRSTAIR DOOR. WHEN THE INTERNAL DOOR HANDLE REACHED THE LOCKING POINT THE HANDLE SHAFT SHEARED. THE DOOR HANDLE HAD BEEN INSTALLED ONLY 49 HOURS (76 CYCLES) PREVIOUS DUE TO THE SAME DEFECT.SDR AUS20020957Handle · sheared(AUS) AIRSTAIR DOOR INTERNAL HANDLE SHAFT SHEARED PREVENTING THE DOOR FROM BEING OPENED FROM THE INSIDE.SDR CA020821002Isolation Mount · debonded(CAN) DURING A ROUTINE INSPECTION OF THE RT ENGINE. THE UPPER INBOARD VIBRATION ISOLATOR ENGINE MOUNT WAS FOUND TO BE DEBONDED, THE BACK HALF OF THE RUBBER WAS DEBONDED FROM THE METAL FACE PLATE. THE MOUNT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA020829008Coupling · worn(CAN) THE INPUT DRIVE SPLINES OF THE ENGINE HIGH PRESSURE FUEL PUMP WERE FOUND TO BE VERY WORN, AND SLIPPAGE OCCURRED CAUSING FUEL STARVATION.SDR AUS20021075Rotor · broken(AUS) RH INNER BRAKE ROTOR BROKEN INTO THREE PIECES.SDR AUS20020894Bulb · burned out(AUS) LANDING GEAR INDICATOR GLOBES (4OFF) UNSERVICEABLE.SDR CA020820004Intake Duct · cracked(CAN) ENGINE AIR INTAKE DUCTS / INERTIA SEPERATORS WERE FOUND TO BE CRACKED PRETTY MUCH ALL OVER. PLEASE NOTE THAT THE PAIR OF AIR INTAKE DUCTS IS CRACKED. THEY ARE MADE OF FIBERGLASS. NEW INTAKES WERE ORDERED AND THE ENGINE AND ENGINE MOUNT HAVE BEEN REMOVSDR CA020821006Breather · chafed(CAN) ENGINE BREATHER ACCESSORIES DRAIN MANIFOLD FOUND CHAFED THROUGH ABOUT 50 PERCENT OF THE TUBE WALL THICKNESS. BREATHER IS CHAFING ON CIRCUMFERENCE OF THE HOLE IT GOES THROUGH IN THE COWLING. THERE IS NO GROMMET, IT IS JUST A HOLE IN THE ALUMINUM SKIN WISDR AUS20020727Windshield · cracked(AUS) RH WINDSHIELD INNER PLY SHATTERED. WINDSHIELD HEAT WAS OFF' AT THE TIME.SDR AUS20020699Flow Divider · faulty(AUS) ENGINE FUEL SYSTEM FLOW DIVIDER FAULTY. IGNITION LEAD ALSO FOUNDTO BE UNSERVICEABLE. ENGINE WAS UNDERGOING GROUND RUNS FOLLOWINGENGINE INSTALLATION. PERSONNEL/MAINTENANCE ERROR.SDR AUS20020670Stud · fractured(AUS) AILERON CONTROL SYSTEM STUD FRACTURED. CLAMP PNO AN737TW56-66 LOOSE AT BOTTOM OF CONTROL COLUMN ALLOWING THE CONTROL COLUMN BOOT PNO 101-54149-37 TO MOVE UNSECURED AROUND THE CONTROLCOLUMN. LH AILERON CONTROL CABLE TURNBUCKLE LOCKWIRE CAUGHT ONBRACKET PNSDR AUS20020648Fuel Tank · collapsed(AUS) RH AUXILIARY FUEL CELL COLLAPSED. VELCRO ATTACHMENT PADS HADBECOME UNGLUED AND SEPARATED FROM THE TOP SURFACE OF THE FUEL CELL. INSPECTION FOUND THAT THE RH FUEL VENT HEATING ELEMENT HADFAILED, ALLOWING THE VENT TO BECOME BLOCKED WITH ICE CAUSING THEFUELSDR 2002FA0000925Brush Block · inoperativeAFTER PROPELLER OVERHAUL AND PROPELLER DE-ICE BRUSH REPLACEMENT, PILOT REPORTED DEICE SYSTEM CIRCUIT/BREAKER SWITCH TRIPPED IN FLIGHT. COULD NOT DUPLICATE PROBLEM ON GROUND WITH ENGINES RUNNING. INSPECTED SYSTEM AND FOUND IF SIDE PRESSURE WS APPLIED TO RIGHSDR AUS20020633Case · corroded(AUS) ENGINE REDUCTION GEARBOX REAR CASE CORRODED BEYOND LIMITS. PAINT HAD BEEN STRIPPED FROM CASE FOR INSPECTION WHEN THE CORROSION WAS FOUND.SDR AUS20020861Bulkhead · cracked(AUS) LOWER REAR PRESSURE BULKHEAD CRACKED. CRACK IS LOCATED IN THE AREA ONE ROW OF RIVETS DOWN FROM THE LAP JOINT AND DIRECTLY ABOVE THE OUTFLOW VALVE. CRACKING IS SIMILAR TO THAT DESCRIBED IN AD/B200/67 BUT WAS NOT FOUND DURING THE AD CHECK. THE AIRCRAFT HASSDR AUS20020710Bolt · cracked(AUS) UPPER FORWARD WING ATTACHMENT BOLT SUSPECT CRACKED. FOUND DURINGFLUORESCENT INSPECTION IAW AD/B200/38 A4 AND BEECH S.I.R.M.SDR AUS20020704Rivet · failed(AUS) AVIONICS SHELF SUPPORT ANGLE RIVET CORRODED AND RIVET HEADSHEARED. RIVET WAS THE FOURTH RIVET FROM THE INBOARD END. FOUND DURING INSPECTION OF FORWARD PRESSURE BULKHEAD LOCATED AT FS 84.SDR AUS20020702Rivet · corroded(AUS) AVIONICS SHELF SUPPORT ANGLE RIVET CORRODED AND RIVET HEADSHEARED. FOUND DURING INSPECTION OF FORWARD PRESSURE BULKHEAD LOCATED AT FS 84.SDR GW12002F00000Line · fracturedPILOT EXPERIENCED LEFT ENGINE ROLL BACK TO IDLE, ENROUTE. INVESTIGATION REVEALED FRACTURED P3 AIR DELIVERY TUBE (PN 3027791) AT THE TUBE/FERRULE JOINT (B) NUT ON THE FUEL CONTROL UNIT. THE P3 TUBE WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERIVCE.SDR AUS20020703Rivet · corroded(AUS) AVIONICS SHELF SUPPORT ANGLE RIVET CORRODED AND RIVET HEADSHEARED. FOUND DURING INSPECTION OF FORWARD PRESSURE BULKHEAD LOCATED AT FS 84.SDR CA020607006Cover · leaking(CAN) STAIN LEAKS WERE FOUND AT THE INBOARD MOST PANEL OF THE RIGHT WING HEADER TANK. THE PANEL IS UNDERNEATH THE WHEEL FAIRING DEFLECTOR. PANEL WAS REMOVED AND RESEALED. SEALER MIGHT HAVE BEEN SLIGHTLY DRY.SDR AUS20020647Lap Joint · scratched(AUS) BULKHEAD LAP JOINT SCRATCHED.SDR VQM2002F00000Fuel Control · malfunctionedPILOT REPORTED LEFT ENGINE TORQUE WAS SLOW TO RESPOND THEN ACCELLERATED RAPIDLY. REPLACED BOTH FUEL CONTROL UNIT AND ENGINE DRIVEN FUEL PUMP (SUSPECTED POSSIBLE BEARING WASH-OUT). PERFORMED GROUND RUNS SATISFACTORY.SDR CA020515012Duct · cracked(CAN) DURING INSPECTION BOTH INERTIA SEPARATORS WERE FOUND CRACKED IN SEVERAL PLACES WITH CRACKS EXTENDING BEYOND 3 INCHES IN EITHER DIRECTIONS. REPLACED.SDR CA020515013Fire Loop · chafed(CAN) DURING INSPECTION OF THE FIRELOOP DETECTION SYSTEM THE FIRELOOP WAS FOUND CHAFING ON THE BAFFLES IN SEVERAL AREAS INCLUDING HEAT EXCHANGER PLUMBING AT ENGINE.SDR YE92002F00001Switch · defectiveLANDING GEAR WAS RETRACTED AFTER TAKEOFF AND LANDING GEAR SEEMED SLUGGISH. LOCAL MAINTENANCE DETERMINED DEFECTIVE GEAR SWITCH. NEW GEAR SWITCH WAS INSTALLED AND TESTED. LANDING GEAR IS OPERATIONAL AT THIS TIME.SDR AUS20020642Arm · failed(AUS) CAPTAINS RH RUDDER PEDAL ARM FAILED. INVESTIGATION FOUND THAT THE PIVOT BOLT HOLE WAS WORN AND ELONGATED.SDR AUS20020357Relay · faulty(AUS) STRETCHER LOADING DEVICE RELAY FAILED.SDR YE92002F00000A/C Pack · malfunctionedPILOT NOTICED CABIN CLIMBING AT A HIGHER THAN NORMAL RATE. AIRCRAFT RETURNED TO AIRPORT AND LOCAL MAINTENANCE DETERMINED. FLOW PACK NEEDED TO BE CHANGED. BOTH FLOW PACKS WERE CHANGED. ALL OPERATIONAL TEST ARE GOOD AT THIS TIME, PRESSURIZATION, NORMAL.SDR AUS20020262Shaft · sheared(AUS) RH ENGINE AIRCONDITIONING COMPRESSOR PULLEY DRIVE QUILL SHAFT SHEARED. LOSS OF ENGINE OIL.SDR EPD2002F00000Windshield · crackedCOCKPIT WINDSHIELD INNER PANEL CRACKED AT ALTITUDE. OUTER PANEL REMAINED INTACT. WINDSHIELD HEAT WAS ON. NO STRIKES NOTED.SDR CTU2002F00004Windshield · crackedCOPILOT WINDSCREEN INNER PANE FAILED AT 27,000 FEET IN LEVEL FLIGHT OUTSIDE AIR TEMPERATURE AT 32 DEGREES. WINDSHIELD (PN 10138402522) (SN 97112H4959) WINDSHIELD INSTALL KIT (PN 101-50413) (SN 21851).SDR AUS20020265Wire · broken(AUS) LANDING GEAR POSITION SYSTEM WIRE BROKEN. WIRE WAS LOCATED IN THE WIRING LOOM IN THE UNDERCARRIAGE BAY.SDR AUS20020325Bolt · loose(AUS) FORWARD RUDDER PUSH-PULL TUBE FORWARD BELLCRANK BOLTS LOOSE.
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